首页> 外国专利> CHANNEL FOR AUTOMATIC TRACKING AIRCRAFTS BY DIRECTION WITH MULTIFUNCTIONAL LONGITUDINAL-MODE SELECTOR AND POSSIBILITY OF AIRCRAFT IDENTIFICATION FOR LASER INFORMATION AND MEASURING SYSTEM OF A LAUNCH-SITE TEST COMPLEX

CHANNEL FOR AUTOMATIC TRACKING AIRCRAFTS BY DIRECTION WITH MULTIFUNCTIONAL LONGITUDINAL-MODE SELECTOR AND POSSIBILITY OF AIRCRAFT IDENTIFICATION FOR LASER INFORMATION AND MEASURING SYSTEM OF A LAUNCH-SITE TEST COMPLEX

机译:多功能纵向模式选择器定向自动跟踪通道和飞机信息识别及发射场测试系统的测量系统

摘要

A channel for automatic tracking of aircrafts by direction with multifunctional longitudinal-mode selector and possibility of aircraft identification for laser information and measuring system of a launch-site test complex includes a control element, a unit for control of deflectors, pumped laser, multi-functional longitudinal-mode selector, block of deflectors, transmitting optics, receiving optics, photodetector, broadband amplifier, multi-functional information block with input b, resonance amplifiers adjusted to respective frequencies of intermode beats, detectors, filters, pulse formers, triggers ("1"|"0"), circuits AND, delay lines, counters, digital-to-analog convertors, low frequency filters, error amplifiers (filters), executive mechanisms and ainput of reference signal with frequency vof transmitting laser, b- input of signal from the channel for estimation of tangent component of velocity (angular velocities) of the aircraft for adjustment of the coincidence error by angles. After error amplifier instead of electronic-digital computing machine a computer is included.
机译:带有多功能纵向模式选择器的定向自动跟踪飞机的通道,以及飞机身份识别的信息,可用于发射场测试综合体的激光信息和测量系统,该通道包括一个控制元件,一个用于控制偏转器的单元,泵浦激光,多个功能性纵向模式选择器,偏转器块,发射光学器件,接收光学器件,光电检测器,宽带放大器,带输入b的多功能信息块,已根据模间差拍的各个频率调整的谐振放大器,检测器,滤波器,脉冲形成器,触发器(“ 1“ |” 0“),电路AND,延迟线,计数器,数模转换器,低频滤波器,误差放大器(滤波器),执行机构和参考频率为v的发射激光的输入,b-输入来自通道的信号,用于估计飞机的速度(角速度)的切线分量,以通过角度调整重合误差。在误差放大器之后而不是电子数字计算机之后,包括一台计算机。

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